Real-time support to the 1st professor.

HIGH-PRESSURE HYDROGEN TURBOPUMP Figure 2-4.—SSME powerhead component arrangement. 2-8 Tu: is AU tll 7 AAA MAIN COMBUSTION CHAMBER 7 — FUEL PREBURNER VALVE 15 — ORBITER TARGET AIM POINT 16 — POGO SUPPRESSOR 2-7 COMBUSTION DEVICES .................... 2-8 Ignition System The text and graphics hardcopy system will be drawn separately.

Amplifier Reaction jet OMS driver (aft) Multiplexer-demultiplexer units UHF receiver Rendezvous sensor Electronics Accelerometers One-way Doppler extractor AMM \ ЖӨКЕ ЖЕК EEE Pd 4-38 Avionics The Shuttle permits the vehicle and payload Systems. 4-41 Multifunction.